Take-off Performance Prediction Using Inertial Data

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Solution Overview

Problem

Current aircraft take-off avionics systems do not provide adequate real-time guidance for pilots to determine the safe take-off speed and refusal point, especially in emergency situations, relying on pilot estimates and assumptions that may be inaccurate.

Innovation Solution

A take-off performance prediction and alerting system that uses inertial data to estimate aircraft weight and acceleration, providing visual and audible notifications to the pilot about the location of safety speeds and reference points along the runway, independent of pilot-entered data and assumptions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If the system uses pilot-entered estimates and assumptions for take-off calculations, then the system complexity is reduced, but the measurement precision and reliability of take-off predictions deteriorate

Engineering Contradiction:
Improvesystem complexityVSAvoidprediction accuracy
Core Design Contradiction:
Device complexityVSMeasurement precision

Solution Approach 1:

The system performs self-measurement of aircraft weight using inertial sensors and on-board equipment data, eliminating the need for manual pilot input. The processor automatically calculates actual weight by comparing inertial data with expected weight based on fuel consumption and payload information, thereby improving prediction accuracy without significantly increasing system complexity.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The system continuously monitors actual acceleration during take-off and compares it with predicted acceleration. This feedback loop allows the system to detect deviations and provide real-time alerts to the pilot, improving the reliability of take-off predictions while maintaining a relatively simple system architecture.

Inventive Principle:
Principle #23Feedback

2Reliability

If the system provides real-time take-off performance monitoring and alerts, then the safety and reliability of take-off operations is improved, but the device complexity increases

Engineering Contradiction:
Improvetake-off safetyVSAvoidsystem complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The system uses existing on-board equipment and inertial sensors for multiple purposes: navigation, performance monitoring, and take-off prediction. By making these existing components multi-functional, the system improves take-off safety without adding significant new hardware or increasing overall system complexity.

Inventive Principle:
Principle #6Universality (Multi-functionality)

Solution Approach 2:

The processor acts as an intermediary that integrates data from various existing systems (inertial sensors, engine parameters, flight management system) to generate take-off performance predictions and alerts. This intermediary approach consolidates multiple functions into a single processing unit, improving reliability while managing system complexity.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Measurement precision

If the system calculates actual aircraft weight using inertial data, then the measurement precision of weight estimation is improved, but the difficulty of detecting and measuring increases

Engineering Contradiction:
Improveweight estimation accuracyVSAvoidweight measurement complexity
Core Design Contradiction:
Measurement precisionVSDifficulty of detecting and measuring

Solution Approach 1:

The system replaces traditional mechanical weight measurement methods (such as scale-based or manual input methods) with inertial-based measurement using onboard sensors. The processor calculates weight by analyzing inertial data and comparing it with expected weight based on fuel consumption and payload information, thereby improving accuracy while managing measurement complexity through computational methods.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Data Source

PatentUS11580864B2Take-off performance prediction and alerting system
Publication Date: 2023.02.14 GULFSTREAM AEROSPACE CORP
  • US11580864B2 patent drawing
  • US11580864B2 patent drawing
  • US11580864B2 patent drawing

AI summary

The aircraft take-off awareness system predicts and informs the pilot about where on the runway certain safety speeds will be achieved. A processor coupled to receive inertial data from the aircraft computes an aircraft weight estimate based at least in part upon the inertial data. The processor then computes a future acceleration prediction based on the computed aircraft weight estimate. Using the future acceleration prediction, the processor then computes the position of various warning reference distances corresponding to predicted positions on the runway at which said certain safety speeds will be achieved. The processor generates a display that it dynamically updates as the reference distances change as the aircraft proceeds down the runway during take-off or aborted take-off.